Two powered-lift concepts, the tandem fan and the longitudinally-arrayed ejector, are integrated with two existing fighter aircraft, the F-l4A and F-16A respectively, to indicate the benefits and/or penalties involved with providing STOVL capability to CTOL aircraft. It is shown that properly designed powered-lift aircraft can achieve either comparable or superior mission performance relative to CTOL aircraft.


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    Titel :

    Supersonic STOVL Research Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Rogers, Al (Autor:in) / Turney, George E. (Autor:in) / Kidwell, George H. (Autor:in) / Wilson, Samuel B. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1982



    Erscheinungsdatum :

    1982-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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